The work summarized in this report is a continuation of NASA's Large-Scale, Swept-Wing Test Articles Fabrication; Research and Test Support for NASA IRT contract (NNC10BA05 -NNC14TA36T) performed by Boeing under the NASA Research and Technology for Aerospace Propulsion Systems (RTAPS) contract. In the study conducted under RTAPS, a series of icing tests in the Icing Research Tunnel (IRT) have been conducted to characterize ice formations on large-scale swept wings representative of modern commercial transport airplanes. The outcome of that campaign was a large database of ice-accretion geometries that can be used for subsequent aerodynamic evaluation in other experimental facilities and for validation of ice-accretion prediction codes.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Icing Simulation Research Supporting the Ice-Accretion Testing of Large-Scale Swept-Wing Models


    Contributors:

    Publication date :

    2018-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Ice-Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel

    Broeren, Andy P. / Potapczuk, Mark G. / Lee, Sam et al. | AIAA | 2016




    Ice-Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel (AIAA 2016-3733)

    Broeren, Andy P. / Potapczuk, Mark G. / Lee, Sam et al. | British Library Conference Proceedings | 2016


    Large-Scale Swept-Wing Icing Simulations in the NASA Glenn Icing Research Tunnel Using LEWICE3D

    Wiberg, Brock D. / Fujiwara, Gustavo E. C. / Woodard, Brian et al. | AIAA | 2014